EP3321721B1 - Strain relief assembly for a fiber optic connector - Google Patents
Strain relief assembly for a fiber optic connector Download PDFInfo
- Publication number
- EP3321721B1 EP3321721B1 EP17201750.1A EP17201750A EP3321721B1 EP 3321721 B1 EP3321721 B1 EP 3321721B1 EP 17201750 A EP17201750 A EP 17201750A EP 3321721 B1 EP3321721 B1 EP 3321721B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- boot
- support
- section
- fiber optic
- optic connector
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Links
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- 230000007423 decrease Effects 0.000 claims description 3
- 230000007704 transition Effects 0.000 description 13
- 230000003287 optical effect Effects 0.000 description 6
- 230000000712 assembly Effects 0.000 description 5
- 238000000429 assembly Methods 0.000 description 5
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- 238000000465 moulding Methods 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 239000004433 Thermoplastic polyurethane Substances 0.000 description 1
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- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
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- 229920001971 elastomer Polymers 0.000 description 1
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Images
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/24—Coupling light guides
- G02B6/36—Mechanical coupling means
- G02B6/38—Mechanical coupling means having fibre to fibre mating means
- G02B6/3807—Dismountable connectors, i.e. comprising plugs
- G02B6/3887—Anchoring optical cables to connector housings, e.g. strain relief features
- G02B6/3888—Protection from over-extension or over-compression
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/44—Mechanical structures for providing tensile strength and external protection for fibres, e.g. optical transmission cables
- G02B6/4439—Auxiliary devices
- G02B6/4471—Terminating devices ; Cable clamps
- G02B6/4477—Terminating devices ; Cable clamps with means for strain-relieving to interior strengths element
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/24—Coupling light guides
- G02B6/36—Mechanical coupling means
- G02B6/38—Mechanical coupling means having fibre to fibre mating means
- G02B6/3807—Dismountable connectors, i.e. comprising plugs
- G02B6/3887—Anchoring optical cables to connector housings, e.g. strain relief features
- G02B6/38875—Protection from bending or twisting
Definitions
- This disclosure relates generally to optical connectivity, and more particularly to strain relief assemblies for fiber optic connectors and fiber optic cable assemblies.
- Optical fibers are useful in a wide variety of applications, including the telecommunications industry for voice, video, and data transmissions.
- a telecommunications system that uses optical fibers
- fiber optic cables that carry the optical fibers connect to equipment or other fiber optic cables.
- fiber optic connectors are often provided on the ends of fiber optic cables.
- the process of terminating individual optical fibers from a fiber optic cable is referred to as "connectorization.” Connectorization can be done in a factory, resulting in a "pre-connectorized” or “pre-terminated” fiber optic cable, or the field (e.g., using a "field-installable” fiber optic connector).
- a fiber optic connector typically includes a ferrule with one or more bores that receive one or more optical fibers.
- the ferrule supports and positions the optical fiber(s) with respect to a housing of the fiber optic connector.
- another connector e.g., in an adapter
- an optical fiber in the ferrule is positioned in a known, fixed location relative to the housing. This allows an optical connection to be established when the optical fiber is aligned with another optical fiber provided in the mating connector.
- the housing and connector bodies (e.g., a retention/crimp body) of a fiber optic connector are often relatively rigid components so that the fiber optic connector can withstand a variety of forces during handling and use without affecting the optical connection that may be or has been established. Having a rigid components, however, presents design challenges elsewhere.
- fiber optic cables upon which fiber optic connectors are installed are typically much less rigid than the connector bodies of the fiber optic connectors. The rapid transition from high stiffness to low stiffness may result in stress concentrations where the cable meets the connector body. Radial loads applied to the cable may then result in the cable bending (e.g., where the stresses are concentrated) beyond a minimum bend radius that must not be exceeded for the cable to function properly.
- a fiber optic connector typically includes a a flexible, strain-relieving boot that snaps onto a rigid portion of the fiber optic connector (e.g., the housing or connector body) and extends rearwardly over a portion of the cable.
- the boot provides a transition in stiffness between the fiber optic connector and the cable.
- US 2015/0036982 A1 discloses a fiber optic connector with a strain relief boot.
- WO2016/115288 A1 discloses a fiber optic connector with a strain relief assembly.
- a fiber optic connector as defined in claim 1.
- a fiber optic connector comprising:
- Embodiments of fiber optic cable assemblies are also provided according to the dependent claims.
- a fiber optic connector 10 not in accordance with the invention also referred to as "optical connector 10", or simply “connector 10"
- Fig. 1 One example of a fiber optic connector 10 not in accordance with the invention (also referred to as "optical connector 10", or simply “connector 10") is shown in Fig. 1 .
- the connector 10 is shown in the form of a SC-type connector, the features described below may be applicable to different connector designs. This includes ST, LC, MU, and MPO-type connectors, for example, and other single-fiber or multi-fiber connector designs.
- the connector 10 includes a ferrule 12 having a ferrule bore 14 ("micro-hole") configured to support an optical fiber 16, a ferrule holder 18 from which the ferrule 12 extends, a housing 20 having a cavity 22 in which the ferrule holder 18 is received, and a connector body 24 (also referred to as “inner housing 24", “retention body 24", or “crimp body 24") configured to retain the ferrule holder 18 within the housing 20.
- a back end 26 of the ferrule 12 is received in a first portion 28 of the ferrule holder 18 and is secured therein in a known manner (e.g., press-fit, adhesive, molding the ferrule holder 18 over the back end 26 of the ferrule 12, etc.).
- the ferrule 12 and ferrule holder 18 may even be a monolithic structure in some embodiments.
- the term "ferrule assembly" may be used to refer to the combination of the ferrule 12 and ferrule holder 18, regardless of whether these elements are separate components secured together or different portions of a monolithic structure.
- the ferrule holder 18 is biased to a forward position within the housing 20 by a spring 32, which extends over a second portion 30 of the ferrule holder 18 that has a reduced cross-sectional diameter/width compared to the first portion 28.
- the spring 32 also interacts with internal geometry of the connector body 24, which may be secured to the housing 20 using a snap-fit or the like.
- Figs. 1 and 2 illustrate a rear portion of the housing 20 having cut-outs or slots 36 on opposite sides so as to define a split shroud.
- the connector body 24 has tabs 38 configured to to be snapped into the slots 36 and retained therein due to the geometries of the components.
- a front end 42 of the ferrule 12 projects beyond a front end 44 of the housing 20.
- the front end 42 presents the optical fiber 16 for optical coupling with a mating component (e.g., another fiber optic connector; not shown).
- a mating component e.g., another fiber optic connector; not shown.
- the ferrule 12 aligns the optical fiber 16 along a longitudinal axis 46.
- Fig. 3 shows how a fiber optic cable 50 (hereinafter "cable 50") including the optical fiber 16 can be terminated with the connector 10.
- the connector 10 can be installed on the cable 50 to form a cable assembly 48.
- the cable 50 is merely an example to facilitate discussion.
- the cable 50 includes an outer jacket 52, inner jacket 54, strength members 56 in the form of aramid yarn, and the optical fiber 16, which itself includes a coating 58 and a buffer layer 60 ("tight buffer"). Portions of the outer jacket 52 and inner jacket 54 have been removed from the optical fiber 16 to expose the strength members 56, which are cut to a desired length and placed over a rear portion 62 of the connector body 24.
- the strength members 56 are coupled to the connector body 24 by a crimp band 64 (also referred to as "crimp ring”) that has been positioned over the optical fiber 16 and a portion of the strength members 56 and inner jacket 54.
- crimp band 64 also referred to as "crimp ring”
- the cable 50 is merely an example, as persons skilled in optical connectivity will appreciate how different cable designs may be terminated with the connector 10.
- the connector body 24 and crimp band 64 are shown in isolation with a strain relief assembly 70 of the connector 10.
- the strain relief assembly 70 is shown exploded from the connector 10 (with the crimp band 64 and cable 50 not shown for clarity).
- the strain relief assembly 70 is positioned over the crimp band 64 and coupled to the connector body 24 when the connector 10 is assembled. More specifically, and with additional reference to Fig. 6 , the strain relief assembly 70 includes a support 72 configured to be coupled to the rear portion 62 of the connector body 24 and a boot 74 received over the support 72.
- the support 72 and boot 74 are formed from respective first and second materials, with the second material being less rigid than the first material.
- the second material may be an elastomer, such as thermoplastic polyurethane
- the first material may be something having a higher modulus of elasticity and/or shear modulus, such as a polycarbonate or metal.
- the support 72 includes a first portion 80 defining a front end 82 of the support 72 and a second portion 84 defining a back end 86 of the support 72.
- An internal cavity 88 extends between the front end 82 and back end 86 and thereby defines a passage through the support 72.
- the first portion 80 represents at least the first quarter of the support 72 in some examples, or at least the first third, first half, or first two-thirds of the support 72 in some examples.
- the first portion 80 is configured to be coupled to the rear portion 62 of the connector body 24.
- One way in which the coupling may be achieved is by designing the dimensions and geometries of the support 72 and connector body 24 to provide a snap-fit connection.
- the embodiment shown in the figures includes inwardly-extending latches or ridges 90 in the internal cavity 88 adjacent the front end 82 of the support 72.
- Slots 92 extending rearwardly from the front end 82 are provided on opposite sides of the first portion 80.
- the slots 92 facilitate the first portion 80 flexing outwardly so that the latches 90 can be moved over a ridge 94 ( Figs. 3-5 ) on the rear portion 64 of the connector body 24.
- the relationship between the ridge 94 and latches 90 helps retain the support 72 (and, therefore, strain relief assembly 70) on the connector body 24 under normal loads.
- the first portion 80 of the support 72 further includes at least one rib 100 (also referred to as a "fin") on an outer surface 102 of the support 72.
- rib 100 also referred to as a "fin"
- Two types of ribs 100 are provided in the example shown.
- First, walls 104 on the support 70 that border the slots 92 may be considered ribs.
- Second, projections 106 on the outer surface 102 that do not border the slots 92 may be considered ribs.
- Four projections 106 are shown in this example: first and second projections 106a, 106b on the side of the first portion including one of the slots 92, and third and fourth projections 106c, 106d on the side of the first portion including the other slot 92.
- the projections 106 are generally planar and aligned (e.g., the first and second projections 106a, 106b are co-planar, as are the third and fourth projections 106c, 106d) or parallel to each other (e.g., the first and second projections 106a, 106b are parallel with the third and fourth projections 106c, 106d).
- Other embodiments may include only one or more walls 104 or only one more projections 106 as the one or more ribs 100, and the ribs need not be aligned and/or parallel when multiple ribs are provided in some embodiments.
- the ribs 100 extend through a wall 108 of the boot 74 when the boot 74 is received over the support 72.
- the second portion 84 of the support 72 has a different geometry than the first portion 80.
- a transition region or portion 110 is defined between the first and second portions 80, 84.
- the second portion 84 has a stiffness less than the first portion 80, which may be achieved by making the second portion 84 shorter in length and/or smaller in diameter/width than the first portion 80.
- the second portion 84 may include structural features along its length that result in lower stiffness than the first portion 80.
- the second portion 84 in the example shown is cylindrical, aligned with the longitudinal axis 46 ( Fig. 1 ), and has a plurality of lateral openings 112 along its length.
- the lateral openings 112 extend in a circumferential direction in the example shown so as to comprise circumferentially-extending slots in the second portion 84.
- the second portion 84 appears "segmented".
- Other shapes and configurations are possible, however. Indeed, in alternative embodiments, the second portion 84 may not have any lateral openings or only have a single lateral opening extending circumferentially and/or axially.
- the boot 74 is substantially longer than (e.g., at least twice the length of) the support 72 and similarly includes at least two sections having different geometries. At least part of the boot 74 that is received over the first portion 80 of the support 72 has a substantially rectangular cross-sectional profile when viewed along the longitudinal axis 46.
- substantially rectangular refers to shapes having four discernible sides at right angles to each other. The sides need not be perfectly planar.
- substantially rectangular may include shapes that are within a region defined by two concentric rectangles. The two concentric rectangles have side edges that differ by less than 20% such that the region is small enough to discern the four sides mentioned above.
- cross-sectional profile refers to the general outline of a cross-section.
- the boot 74 extends rearwardly from the support 72 and eventually terminates with a circular or substantially circular or otherwise round profile when viewed along the longitudinal axis 46. Accordingly, the boot 74 transitions from the rectangular or substantially rectangular profile to the round or substantially round profile as the boot 74 extends rearwardly from the first portion 80 of the support 72.
- substantially round refers to shapes that are within a region defined by two concentric circles or ellipses. The two circles or ellipses have radial dimensions that differ by less than 20%.
- the boot 74 may be over-molded onto the support 72 to be received thereon, although other methods of securing the boot 74 to the support 72 will be appreciated. Regardless of how the boot 74 is formed, the boot 74 includes an internal passageway communicating with the internal cavity of the support. Together, the internal cavity and internal passageway define a passage through the strain relief assembly.
- the rib(s) 100 on the first portion 80 of the support 72 extend through a wall 108 of the boot 74 at one or more locations.
- Fig. 7 which illustrates the connector 10 in an assembled condition and partially in cross-section.
- the connector 10 may further include a shroud 120 received over the housing 20, connector body 24, and at least a portion of the strain relief assembly 70.
- the shroud 120 in the particular embodiment shown extends over the entire first portion 80 of the support 72 and, therefore, the section of the boot 74 that is received over the first portion 80.
- the boot 74 extends from the front end 82 of the support 72 and rearwardly over the first portion 80 in the embodiment shown, but other arrangements are possible.
- the boot 74 is received over at least 75% of the first portion 80 of the support 72. Regardless, at least some of the boot 74 is positioned between the first portion 80 of the support 72 and the shroud 120. Inner surfaces 122 of the shroud 120 confront the outer surfaces 124 ( Fig. 6 ) of the boot 74. Each rib 100 on the first portion 80 of the support 72 extends through the wall 108 of the boot 74 toward one of the inner surfaces 122. In some embodiments, the ribs 100 may even contact the associated inner surface 122 of the shroud 120.
- the ribs 100 allow forces to be effectively transferred to the shroud 120 during use. For example, when a radial/side load is applied to the cable 50 ( Fig. 3 ), the coupling between the strain relief assembly 70 and connector body 24 may experience less stress due to the force transfer to the shroud 120. This reduces the likelihood of the strain relief assembly 70 bending or otherwise deforming beyond an acceptable level (e.g., the minimum bend radius of the optical fiber 16).
- the ribs 100 may be one feature that increases the support capability of the strain relief assembly 70 compared to conventional designs, on a more general level simply providing the strain relief assembly 70 with components formed from different materials-one being more rigid than the other-offers advantages with respect to stiffness.
- the rigid first material of the support 72 helps ensure that the portion of the strain relief assembly 70 that couples to the connector body 24 has a relatively high stiffness. This avoids a significant/sharp transition in stiffness between the connector body 24 and strain relief assembly 70, thereby reducing the concentration of stresses at the coupling when the cable 50 experiences side loads or other forces.
- the relatively high stiffness can be provided without sacrificing a smooth transition in stiffness at the other end of the strain relief assembly 70 between the end of the boot 74 and the cable 50.
- the strain relief assembly 70 is still able to transition to a sufficiently low stiffness in an acceptable amount of length due to its construction.
- the geometry of the support 72 is such that the second portion 84 has a lower stiffness than the first portion 80, thereby providing a transition in stiffness between the rigid material of the support 72 and the less rigid material of the boot 74.
- the boot 74 is provided with a different geometry.
- a fiber optic connector 200 (“connector 200") with an alternative strain relief assembly 202 is shown in Figs. 8 and 9 .
- the strain relief 202 assembly includes the support 72 and a boot 204 that bulges radially outward as the boot 204 extends over the back end 86 of the support 72.
- the boot 204 may be received on the support 74 in the same manner as the boot.
- the description above for the connector 10-including the potential variations- applies equally the connector 200, and the same reference numbers are used in the figures to refer to corresponding elements. To simplify matters, only the different geometry of the boot 204 will be described.
- the boot 204 includes an internal passageway 210 arranged about a central axis, which may correspond to the longitudinal axis 46 when the connector 200 is assembled.
- reference number 46 will be used to refer to both the central axis of the boot 204 and the longitudinal axis of the connector 200 even though embodiments are possible where the central axis may not exactly correspond to the longitudinal axis.
- the internal passageway 210 communicates with the internal cavity 88 of the support 72. Together, the internal passageway 210 and internal cavity 88 define the internal passage through the strain relief assembly 202.
- the boot 204 flares radially outward from the central axis 46 as the boot 204 extends over the second portion 84 of the support 72 and toward the back end 86 of the support 72. Additionally, all or part of the boot 204 tapers radially inward toward the central axis 46 as the boot 204 extends rearwardly from the back end 86 of the support 72. The extent of the flare radially outward and the taper radially inward depends on the particular embodiment.
- the boot 204 can be considered to have a width in a plane perpendicular to the central axis 46 ("transverse plane"), with the width being measured through the central axis 46. The width corresponds to an outer diameter when the boot 204 has a substantially round cross-sectional profile in the transverse plane. The width may correspond to a bisecting line when the boot 204 has a substantially rectangular cross-sectional profile in the transverse plane.
- the part(s) of the boot 204 that flare radially outward from the central axis 46 may increase in width by at least 20%. Also, in some embodiments, the part(s) of the boot 204 that taper radially inward toward the central axis 46 may decrease in width by at least 50%.
- the sections of the boot 204 extending over and rearwardly from the second portion 84 of the support 72 have a substantially round tubular configuration (i.e., a tubular configuration that has substantially round cross-sectional profiles when viewed along the central axis 46 at different axial locations).
- a small section of the boot 204 flares radially outward from the central axis 46, and then a long section of the boot 204 (e.g., substantially the remaining length of the boot 204) tapers radially inward toward the central axis 46.
- the width of the boot 204 is greatest at a location along the boot 204 that substantially corresponds to where the boot 204 extends over the back end 86 of the support 72. The same may be true in embodiments where the boot 204 flares radially outward and tapers radially inward in a different manner.
- Fig. 10 is a perspective view of the strain relief assembly 202 in isolation.
- Figs. 11, 12, and 13 are respective top plan, side elevation, and front elevation views of the strain relief assembly 202.
- the boot 204 includes a first section 220 extending over the first portion 80 of the support 72, a second section 222 extending over the second portion 84 of the support 72, and a third section 224 extending rearwardly from the back end 86 of the support 72.
- the first section 220, second section 222, and third section 224 have different tubular configurations.
- the first section 220, second section 222, and third section 224 are each tube-like (e.g., each defines a portion of the internal passageway 210), yet the shapes of the tubes are different.
- the first section 220 has a substantially rectangular tubular configuration as discussed above.
- Four corners 228 are clearly defined by the substantially rectangular tubular configuration, even though the corners 228 are rounded in the particular embodiment shown. Additionally, even though the first section 220 may include rounded portions or humps 230 on sides between the four corners 228, the first section 220 is still considered to have a substantially rectangular cross-sectional profile when viewed along the central axis 46.
- substantially rectangular refers to a shape that fits within two concentric rectangles whose side edges differ in length by less than 20%.
- FIG. 13 illustrates how the plurality of ribs/fins 100 on the first portion 80 of the support 72 extend through the first section 220 of the boot 204.
- the ribs 100 define four corner regions 232 in the first section 220 of the boot 204.
- the corner regions 232 include the respective corners 228 in the embodiment shown.
- the first section 220 may not have a substantially rectangular tubular configuration yet still include corner regions defined between the ribs 100 on the first portion 80 of the support 72.
- the second section 222 of the boot 204 has the substantially round tubular configuration mentioned above in connection with Figs. 8 and 9 . More specifically, in the embodiment shown, the second section 222 includes a neck portion 236 and a flared portion 238 as the second section 222 extends over the second portion 84 of the support 72.
- the neck portion 236 maintains a substantially constant cross-sectional profile when viewed along the central axis 46. Indeed, the neck portion 236 in the embodiment shown has a substantially cylindrical tubular configuration.
- the flared portion 238 increases the diameter of the second section 222 to provide a transition between the neck portion 236 and the location where the boot 204 has a maximum width. That location, as mentioned above, may substantially correspond to where the boot 204 extends over the back end 86 of the support 72.
- the neck portion 236 and the flared portion 238 of the second section 222 have respective first and second lengths Li, L 2 measured along the central axis 46.
- the first length L 1 is greater than the second length L 2 in the embodiment shown, but in other embodiments the flared portion 238 may be longer than the neck portion 236. Indeed, in some embodiments, the entire length of the second section 222 may be flared such that there is no neck portion.
- the third section 224 of the boot 204 defines a distal or terminal end 242 of the boot 204. Similar to the second section 222, the third section 224 has the substantially round tubular configuration mentioned above in connection with Figs. 8 and 9 . The third section 224 gradually tapers radially inward toward the central axis 46 such that the round tubular configuration decreases in diameter along substantially all of the length of the third section 224.
- the "flared” or “bulged” shaped of the boot 204 may help improve the transition in stiffness between the support 72 and the boot 204, as mentioned above. As a result, the strain relief assembly 202 may be less likely to experience unacceptable stress concentrations when subjected to side loads or the like.
- FIGs. 14 and 15 illustrate a fiber optic connector 300 ("connector 300") with a strain relief assembly 302 similar to the strain relief assembly 202.
- the second section 222 of the boot 204 in the strain relief assembly 302 includes ribs 306 extending along a length of the second section 222.
- ribs 306 are provided in the embodiment shown, with each of the ribs 306 being circumferentially aligned with one of the corners 228 of the first section 220 of the boot 204.
- each of the ribs 306 may or may not be circumferentially aligned with one of the corners 228. Similar statements apply with respect to the corner regions 232. That is, each of the ribs 306 is circumferentially aligned with one of the corner regions 232 in the embodiment shown, but there may more or less ribs 306 in alternative embodiments that may or may not be aligned with the corner regions 232 of the first section 220.
- the shroud 120 of the connectors 10, 200, 300 may be a conventional shroud, and the strain relief assemblies 70, 202, 302 may be comparable in size to a conventional, monolithic strain relief structure (e.g., an elastomeric boot alone). Over-molding the boots 74, 204 onto the support 72 is one way to achieve this advantage.
- a sufficient length of the boot is positioned between the first portion 80 of the support 72 and the shroud 120 so that the overall length of the strain relief assembly 70 is not significantly increased, if at all, compared to conventional designs.
- the boots 74, 204 extend from the front end 82 of the support 72 and rearwardly over the first and second portions 80, 84. In other embodiments, the boots 74, 204 may be received over the support 72 to a lesser extent. The boots 74, 204 are received over at least 75% of the first portion 80.
Description
- This disclosure relates generally to optical connectivity, and more particularly to strain relief assemblies for fiber optic connectors and fiber optic cable assemblies.
- Optical fibers are useful in a wide variety of applications, including the telecommunications industry for voice, video, and data transmissions. In a telecommunications system that uses optical fibers, there are typically many locations where fiber optic cables that carry the optical fibers connect to equipment or other fiber optic cables. To conveniently provide these connections, fiber optic connectors are often provided on the ends of fiber optic cables. The process of terminating individual optical fibers from a fiber optic cable is referred to as "connectorization." Connectorization can be done in a factory, resulting in a "pre-connectorized" or "pre-terminated" fiber optic cable, or the field (e.g., using a "field-installable" fiber optic connector).
- Regardless of where installation occurs, a fiber optic connector typically includes a ferrule with one or more bores that receive one or more optical fibers. The ferrule supports and positions the optical fiber(s) with respect to a housing of the fiber optic connector. Thus, when the housing of the fiber optic connector is mated with another connector (e.g., in an adapter), an optical fiber in the ferrule is positioned in a known, fixed location relative to the housing. This allows an optical connection to be established when the optical fiber is aligned with another optical fiber provided in the mating connector.
- The housing and connector bodies (e.g., a retention/crimp body) of a fiber optic connector are often relatively rigid components so that the fiber optic connector can withstand a variety of forces during handling and use without affecting the optical connection that may be or has been established. Having a rigid components, however, presents design challenges elsewhere. For example, fiber optic cables upon which fiber optic connectors are installed are typically much less rigid than the connector bodies of the fiber optic connectors. The rapid transition from high stiffness to low stiffness may result in stress concentrations where the cable meets the connector body. Radial loads applied to the cable may then result in the cable bending (e.g., where the stresses are concentrated) beyond a minimum bend radius that must not be exceeded for the cable to function properly.
- To address the above-mentioned challenge, a fiber optic connector typically includes a a flexible, strain-relieving boot that snaps onto a rigid portion of the fiber optic connector (e.g., the housing or connector body) and extends rearwardly over a portion of the cable. The boot provides a transition in stiffness between the fiber optic connector and the cable. Although many different boot designs have been proposed to properly provide this transition, new solutions are still desired. It can be difficult to address conflicting conditions at opposite ends of the boot, namely a high stiffness at the end of the boot coupled to the connector and a low stiffness at the end of the boot terminating on the cable. Failure to do so may result in stress concentration points that weaken the boot or otherwise still lead to unacceptable bending of the cable. Existing solutions may not adequately address these conflicting conditions, manufacturability challenges, space constraints, and other considerations.
US 2015/0036982 A1 discloses a fiber optic connector with a strain relief boot.WO2016/115288 A1 discloses a fiber optic connector with a strain relief assembly. - According to a first aspect of the invention; there is provided a fiber optic connector as defined in claim 1. A fiber optic connector, comprising:
- a ferrule configured to support at least one optical fiber;
- a housing from which the ferrule extends;
- a ferrule holder supporting the ferrule within the housing;
- a connector body coupled to the housing and configured to retain the ferrule holder within the housing, the connector body having a rear portion at least partially outside of the housing;
- a crimp band coupling strength members of a fiber optic cable to the connector body, wherein the crimp band is positioned over a portion of the strength members and an inner jacket of the fiber optic cable; and
- a strain relief assembly positioned over the crimp band and coupled to the connector body, the strain relief assembly comprising: a support having a front end, a back end, and an internal cavity extending between the front end and the back end, wherein the support of the strain relief assembly is coupled to the rear portion of the connector body such that the strain relief assembly is coupled to the housing by the connector body; and a boot extending over at least 75% of the support and rearwardly from the back end; wherein: the support is formed from a first material and the boot is formed from a second material that is less rigid than the first material; and the boot includes an internal passageway arranged about a central axis and communicating with the internal cavity of the support, characterised in that: at least part of the boot flares radially outward from the central axis as the boot extends over the at least a portion of the support toward the back end of the support; and at least part of the boot tapers radially inward toward the central axis as the boot extends rearwardly from the back end of the support.
- Embodiments of fiber optic cable assemblies are also provided according to the dependent claims.
- The accompanying drawings are included to provide a further understanding, and are incorporated in and constitute a part of this specification. The drawings illustrate one or more embodiment(s), and together with the description serve to explain principles and operation of the various embodiments. Features and attributes associated with any of the embodiments shown or described may be applied to other embodiments shown, described, or appreciated based on this disclosure.
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Fig. 1 a perspective view of an example of a fiber optic connector; -
Fig. 2 is an exploded perspective view the fiber optic connector ofFig. 1 ; -
Fig. 3 is schematic cross-sectional view the fiber optic connector ofFig. 1 installed onto a fiber optic cable; -
Fig. 4 is an exploded perspective view of a connector body, crimp band, and strain relief assembly for the fiber optic connector ofFig. 1 ; -
Fig. 5 is a perspective view similar toFig. 1 , but additionally showing the strain relief assembly ofFig. 4 exploded from the fiber optic connector; -
Fig. 6 is an exploded perspective of the strain relief assembly ofFig. 4 ; -
Fig. 7 is a perspective view, partially in cross-section, of the fiber optic connector ofFig. 1 including the strain relief assembly ofFig. 4 and a shroud; -
Fig. 8 is a side elevation view of a fiber optic connector according to another embodiment; -
Fig. 9 is a cross-sectional view of the fiber optic connector ofFig. 8 ; -
Fig. 10 is a perspective view of a strain relief assembly in the fiber optic connector ofFig. 8 ; -
Fig. 11 is a top plan view of the strain relief assembly ofFig. 10 ; -
Fig. 12 is a side elevation view of the strain relief assembly ofFig. 10 ; -
Fig. 13 is a front elevation view of the strain relief assembly ofFig. 10 ; -
Fig. 14 is a side elevation view of a fiber optic connector according to yet another embodiment; and -
Fig. 15 is a perspective view, partially cut-away, of a strain relief assembly in the fiber optic connector ofFig. 14 . - Various embodiments will be further clarified by examples in the description below. In general, the description relates fiber optic connectors and cable assemblies including the same. One example of a fiber
optic connector 10 not in accordance with the invention (also referred to as "optical connector 10", or simply "connector 10") is shown inFig. 1 . Although theconnector 10 is shown in the form of a SC-type connector, the features described below may be applicable to different connector designs. This includes ST, LC, MU, and MPO-type connectors, for example, and other single-fiber or multi-fiber connector designs. - As shown in
Figs. 1 and 2 , theconnector 10 includes aferrule 12 having a ferrule bore 14 ("micro-hole") configured to support anoptical fiber 16, aferrule holder 18 from which theferrule 12 extends, ahousing 20 having acavity 22 in which theferrule holder 18 is received, and a connector body 24 (also referred to as "inner housing 24", "retention body 24", or "crimp body 24") configured to retain theferrule holder 18 within thehousing 20. More specifically, aback end 26 of theferrule 12 is received in afirst portion 28 of theferrule holder 18 and is secured therein in a known manner (e.g., press-fit, adhesive, molding theferrule holder 18 over theback end 26 of theferrule 12, etc.). Theferrule 12 andferrule holder 18 may even be a monolithic structure in some embodiments. For convenience, the term "ferrule assembly" may be used to refer to the combination of theferrule 12 andferrule holder 18, regardless of whether these elements are separate components secured together or different portions of a monolithic structure. - The
ferrule holder 18 is biased to a forward position within thehousing 20 by aspring 32, which extends over asecond portion 30 of theferrule holder 18 that has a reduced cross-sectional diameter/width compared to thefirst portion 28. Thespring 32 also interacts with internal geometry of theconnector body 24, which may be secured to thehousing 20 using a snap-fit or the like. For example,Figs. 1 and 2 illustrate a rear portion of thehousing 20 having cut-outs orslots 36 on opposite sides so as to define a split shroud. Theconnector body 24 hastabs 38 configured to to be snapped into theslots 36 and retained therein due to the geometries of the components. - When the
connector 10 is assembled as shown inFig. 1 , afront end 42 of theferrule 12 projects beyond afront end 44 of thehousing 20. Thefront end 42 presents theoptical fiber 16 for optical coupling with a mating component (e.g., another fiber optic connector; not shown). Note that theferrule 12 aligns theoptical fiber 16 along alongitudinal axis 46. These aspects can be better appreciated with reference toFig. 3 , which shows how a fiber optic cable 50 (hereinafter "cable 50") including theoptical fiber 16 can be terminated with theconnector 10. In other words, theconnector 10 can be installed on thecable 50 to form acable assembly 48. Thecable 50 is merely an example to facilitate discussion. In the example shown, thecable 50 includes anouter jacket 52,inner jacket 54,strength members 56 in the form of aramid yarn, and theoptical fiber 16, which itself includes acoating 58 and a buffer layer 60 ("tight buffer"). Portions of theouter jacket 52 andinner jacket 54 have been removed from theoptical fiber 16 to expose thestrength members 56, which are cut to a desired length and placed over arear portion 62 of theconnector body 24. Thestrength members 56 are coupled to theconnector body 24 by a crimp band 64 (also referred to as "crimp ring") that has been positioned over theoptical fiber 16 and a portion of thestrength members 56 andinner jacket 54. Again, thecable 50 is merely an example, as persons skilled in optical connectivity will appreciate how different cable designs may be terminated with theconnector 10. - In
Fig. 4 , theconnector body 24 and crimpband 64 are shown in isolation with astrain relief assembly 70 of theconnector 10. InFig. 5 , thestrain relief assembly 70 is shown exploded from the connector 10 (with thecrimp band 64 andcable 50 not shown for clarity). Thestrain relief assembly 70 is positioned over thecrimp band 64 and coupled to theconnector body 24 when theconnector 10 is assembled. More specifically, and with additional reference toFig. 6 , thestrain relief assembly 70 includes asupport 72 configured to be coupled to therear portion 62 of theconnector body 24 and aboot 74 received over thesupport 72. Thesupport 72 andboot 74 are formed from respective first and second materials, with the second material being less rigid than the first material. For example, in some embodiments the second material may be an elastomer, such as thermoplastic polyurethane, and the first material may be something having a higher modulus of elasticity and/or shear modulus, such as a polycarbonate or metal. The advantages of such an arrangement will be apparent after further describing other aspects of thestrain relief assembly 70 below. - Referring specifically to
Fig. 6 , thesupport 72 includes afirst portion 80 defining afront end 82 of thesupport 72 and asecond portion 84 defining aback end 86 of thesupport 72. Aninternal cavity 88 extends between thefront end 82 andback end 86 and thereby defines a passage through thesupport 72. Thefirst portion 80 represents at least the first quarter of thesupport 72 in some examples, or at least the first third, first half, or first two-thirds of thesupport 72 in some examples. To this end, thefirst portion 80 is configured to be coupled to therear portion 62 of theconnector body 24. One way in which the coupling may be achieved is by designing the dimensions and geometries of thesupport 72 andconnector body 24 to provide a snap-fit connection. For example, the embodiment shown in the figures includes inwardly-extending latches orridges 90 in theinternal cavity 88 adjacent thefront end 82 of thesupport 72.Slots 92 extending rearwardly from thefront end 82 are provided on opposite sides of thefirst portion 80. Theslots 92 facilitate thefirst portion 80 flexing outwardly so that thelatches 90 can be moved over a ridge 94 (Figs. 3-5 ) on therear portion 64 of theconnector body 24. The relationship between theridge 94 and latches 90 helps retain the support 72 (and, therefore, strain relief assembly 70) on theconnector body 24 under normal loads. - The
first portion 80 of thesupport 72 further includes at least one rib 100 (also referred to as a "fin") on anouter surface 102 of thesupport 72. Two types ofribs 100 are provided in the example shown. First, walls 104 on thesupport 70 that border theslots 92 may be considered ribs. Second, projections 106 on theouter surface 102 that do not border theslots 92 may be considered ribs. Four projections 106 are shown in this example: first andsecond projections 106a, 106b on the side of the first portion including one of theslots 92, and third andfourth projections other slot 92. The projections 106 are generally planar and aligned (e.g., the first andsecond projections 106a, 106b are co-planar, as are the third andfourth projections second projections 106a, 106b are parallel with the third andfourth projections more ribs 100, and the ribs need not be aligned and/or parallel when multiple ribs are provided in some embodiments. As will be described in greater detail below, theribs 100 extend through awall 108 of theboot 74 when theboot 74 is received over thesupport 72. - Still referring to
Fig. 6 , thesecond portion 84 of thesupport 72 has a different geometry than thefirst portion 80. As such, a transition region orportion 110 is defined between the first andsecond portions second portion 84 has a stiffness less than thefirst portion 80, which may be achieved by making thesecond portion 84 shorter in length and/or smaller in diameter/width than thefirst portion 80. Additionally, thesecond portion 84 may include structural features along its length that result in lower stiffness than thefirst portion 80. For example, thesecond portion 84 in the example shown is cylindrical, aligned with the longitudinal axis 46 (Fig. 1 ), and has a plurality oflateral openings 112 along its length. Thelateral openings 112 extend in a circumferential direction in the example shown so as to comprise circumferentially-extending slots in thesecond portion 84. To this end, thesecond portion 84 appears "segmented". Other shapes and configurations are possible, however. Indeed, in alternative embodiments, thesecond portion 84 may not have any lateral openings or only have a single lateral opening extending circumferentially and/or axially. - Now referring to both
Figs. 5 and 6 , theboot 74 is substantially longer than (e.g., at least twice the length of) thesupport 72 and similarly includes at least two sections having different geometries. At least part of theboot 74 that is received over thefirst portion 80 of thesupport 72 has a substantially rectangular cross-sectional profile when viewed along thelongitudinal axis 46. As used herein, "substantially rectangular" refers to shapes having four discernible sides at right angles to each other. The sides need not be perfectly planar. For example, "substantially rectangular" may include shapes that are within a region defined by two concentric rectangles. The two concentric rectangles have side edges that differ by less than 20% such that the region is small enough to discern the four sides mentioned above. Additionally, cross-sectional profile refers to the general outline of a cross-section. - Still referring to
Figs. 5 and 6 , theboot 74 extends rearwardly from thesupport 72 and eventually terminates with a circular or substantially circular or otherwise round profile when viewed along thelongitudinal axis 46. Accordingly, theboot 74 transitions from the rectangular or substantially rectangular profile to the round or substantially round profile as theboot 74 extends rearwardly from thefirst portion 80 of thesupport 72. As used herein, "substantially round" refers to shapes that are within a region defined by two concentric circles or ellipses. The two circles or ellipses have radial dimensions that differ by less than 20%. - The
boot 74 may be over-molded onto thesupport 72 to be received thereon, although other methods of securing theboot 74 to thesupport 72 will be appreciated. Regardless of how theboot 74 is formed, theboot 74 includes an internal passageway communicating with the internal cavity of the support. Together, the internal cavity and internal passageway define a passage through the strain relief assembly. - As mentioned above, the rib(s) 100 on the
first portion 80 of thesupport 72 extend through awall 108 of theboot 74 at one or more locations. This can be better appreciated with reference toFig. 7 , which illustrates theconnector 10 in an assembled condition and partially in cross-section. As shown inFig. 7 , theconnector 10 may further include ashroud 120 received over thehousing 20,connector body 24, and at least a portion of thestrain relief assembly 70. Theshroud 120 in the particular embodiment shown extends over the entirefirst portion 80 of thesupport 72 and, therefore, the section of theboot 74 that is received over thefirst portion 80. Theboot 74 extends from thefront end 82 of thesupport 72 and rearwardly over thefirst portion 80 in the embodiment shown, but other arrangements are possible. Theboot 74 is received over at least 75% of thefirst portion 80 of thesupport 72. Regardless, at least some of theboot 74 is positioned between thefirst portion 80 of thesupport 72 and theshroud 120.Inner surfaces 122 of theshroud 120 confront the outer surfaces 124 (Fig. 6 ) of theboot 74. Eachrib 100 on thefirst portion 80 of thesupport 72 extends through thewall 108 of theboot 74 toward one of theinner surfaces 122. In some embodiments, theribs 100 may even contact the associatedinner surface 122 of theshroud 120. - By extending to or beyond an outer surface of the
boot 74, theribs 100 allow forces to be effectively transferred to theshroud 120 during use. For example, when a radial/side load is applied to the cable 50 (Fig. 3 ), the coupling between thestrain relief assembly 70 andconnector body 24 may experience less stress due to the force transfer to theshroud 120. This reduces the likelihood of thestrain relief assembly 70 bending or otherwise deforming beyond an acceptable level (e.g., the minimum bend radius of the optical fiber 16). - Although the
ribs 100 may be one feature that increases the support capability of thestrain relief assembly 70 compared to conventional designs, on a more general level simply providing thestrain relief assembly 70 with components formed from different materials-one being more rigid than the other-offers advantages with respect to stiffness. In particular, the rigid first material of thesupport 72 helps ensure that the portion of thestrain relief assembly 70 that couples to theconnector body 24 has a relatively high stiffness. This avoids a significant/sharp transition in stiffness between theconnector body 24 andstrain relief assembly 70, thereby reducing the concentration of stresses at the coupling when thecable 50 experiences side loads or other forces. - Moreover, the relatively high stiffness can be provided without sacrificing a smooth transition in stiffness at the other end of the
strain relief assembly 70 between the end of theboot 74 and thecable 50. In other words, thestrain relief assembly 70 is still able to transition to a sufficiently low stiffness in an acceptable amount of length due to its construction. The geometry of thesupport 72 is such that thesecond portion 84 has a lower stiffness than thefirst portion 80, thereby providing a transition in stiffness between the rigid material of thesupport 72 and the less rigid material of theboot 74. Thus, within thestrain relief assembly 70 itself, the potential for stress concentrations due to sharp transitions in stiffness between thesupport 72 andboot 74 is reduced/minimized. - To even further improve the transition in stiffness between the
support 72 and theboot 74, theboot 74 is provided with a different geometry. One embodiment of a fiber optic connector 200 ("connector 200") with an alternativestrain relief assembly 202 is shown inFigs. 8 and 9 . Thestrain relief 202 assembly includes thesupport 72 and aboot 204 that bulges radially outward as theboot 204 extends over theback end 86 of thesupport 72. Theboot 204 may be received on thesupport 74 in the same manner as the boot. Indeed, the description above for the connector 10-including the potential variations- applies equally theconnector 200, and the same reference numbers are used in the figures to refer to corresponding elements. To simplify matters, only the different geometry of theboot 204 will be described. - As shown in
Fig. 9 , theboot 204 includes aninternal passageway 210 arranged about a central axis, which may correspond to thelongitudinal axis 46 when theconnector 200 is assembled. For convenience,reference number 46 will be used to refer to both the central axis of theboot 204 and the longitudinal axis of theconnector 200 even though embodiments are possible where the central axis may not exactly correspond to the longitudinal axis. Theinternal passageway 210 communicates with theinternal cavity 88 of thesupport 72. Together, theinternal passageway 210 andinternal cavity 88 define the internal passage through thestrain relief assembly 202. - In the embodiment shown in
Figs. 8 and 9 , at least part of theboot 204 flares radially outward from thecentral axis 46 as theboot 204 extends over thesecond portion 84 of thesupport 72 and toward theback end 86 of thesupport 72. Additionally, all or part of theboot 204 tapers radially inward toward thecentral axis 46 as theboot 204 extends rearwardly from theback end 86 of thesupport 72. The extent of the flare radially outward and the taper radially inward depends on the particular embodiment. For example, theboot 204 can be considered to have a width in a plane perpendicular to the central axis 46 ("transverse plane"), with the width being measured through thecentral axis 46. The width corresponds to an outer diameter when theboot 204 has a substantially round cross-sectional profile in the transverse plane. The width may correspond to a bisecting line when theboot 204 has a substantially rectangular cross-sectional profile in the transverse plane. - In some embodiments, the part(s) of the
boot 204 that flare radially outward from thecentral axis 46 may increase in width by at least 20%. Also, in some embodiments, the part(s) of theboot 204 that taper radially inward toward thecentral axis 46 may decrease in width by at least 50%. In the embodiment shown inFigs. 8 and 9 , the sections of theboot 204 extending over and rearwardly from thesecond portion 84 of thesupport 72 have a substantially round tubular configuration (i.e., a tubular configuration that has substantially round cross-sectional profiles when viewed along thecentral axis 46 at different axial locations). A small section of theboot 204 flares radially outward from thecentral axis 46, and then a long section of the boot 204 (e.g., substantially the remaining length of the boot 204) tapers radially inward toward thecentral axis 46. The width of theboot 204 is greatest at a location along theboot 204 that substantially corresponds to where theboot 204 extends over theback end 86 of thesupport 72. The same may be true in embodiments where theboot 204 flares radially outward and tapers radially inward in a different manner. - To further characterize the different geometry of the
boot 204, reference will now be additionally made toFigs. 10-13 .Fig. 10 is a perspective view of thestrain relief assembly 202 in isolation.Figs. 11, 12, and 13 are respective top plan, side elevation, and front elevation views of thestrain relief assembly 202. - As shown in
Figs. 8-13 , theboot 204 includes afirst section 220 extending over thefirst portion 80 of thesupport 72, asecond section 222 extending over thesecond portion 84 of thesupport 72, and athird section 224 extending rearwardly from theback end 86 of thesupport 72. Thefirst section 220,second section 222, andthird section 224 have different tubular configurations. In other words, thefirst section 220,second section 222, andthird section 224 are each tube-like (e.g., each defines a portion of the internal passageway 210), yet the shapes of the tubes are different. - In the embodiment shown, the
first section 220 has a substantially rectangular tubular configuration as discussed above. Fourcorners 228 are clearly defined by the substantially rectangular tubular configuration, even though thecorners 228 are rounded in the particular embodiment shown. Additionally, even though thefirst section 220 may include rounded portions orhumps 230 on sides between the fourcorners 228, thefirst section 220 is still considered to have a substantially rectangular cross-sectional profile when viewed along thecentral axis 46. As mentioned above, "substantially rectangular" refers to a shape that fits within two concentric rectangles whose side edges differ in length by less than 20%. - An additional or alternative way to characterize the shape of the
first section 220 of theboot 204 may include reference to thesupport 72. For example,Fig. 13 illustrates how the plurality of ribs/fins 100 on thefirst portion 80 of thesupport 72 extend through thefirst section 220 of theboot 204. Theribs 100 define fourcorner regions 232 in thefirst section 220 of theboot 204. Thecorner regions 232 include therespective corners 228 in the embodiment shown. In alternative embodiments, thefirst section 220 may not have a substantially rectangular tubular configuration yet still include corner regions defined between theribs 100 on thefirst portion 80 of thesupport 72. - Now referring to
Figs. 11 and 12 , thesecond section 222 of theboot 204 has the substantially round tubular configuration mentioned above in connection withFigs. 8 and 9 . More specifically, in the embodiment shown, thesecond section 222 includes aneck portion 236 and a flaredportion 238 as thesecond section 222 extends over thesecond portion 84 of thesupport 72. Theneck portion 236 maintains a substantially constant cross-sectional profile when viewed along thecentral axis 46. Indeed, theneck portion 236 in the embodiment shown has a substantially cylindrical tubular configuration. The flaredportion 238 increases the diameter of thesecond section 222 to provide a transition between theneck portion 236 and the location where theboot 204 has a maximum width. That location, as mentioned above, may substantially correspond to where theboot 204 extends over theback end 86 of thesupport 72. - The
neck portion 236 and the flaredportion 238 of thesecond section 222 have respective first and second lengths Li, L2 measured along thecentral axis 46. The first length L1 is greater than the second length L2 in the embodiment shown, but in other embodiments the flaredportion 238 may be longer than theneck portion 236. Indeed, in some embodiments, the entire length of thesecond section 222 may be flared such that there is no neck portion. - The
third section 224 of theboot 204 defines a distal orterminal end 242 of theboot 204. Similar to thesecond section 222, thethird section 224 has the substantially round tubular configuration mentioned above in connection withFigs. 8 and 9 . Thethird section 224 gradually tapers radially inward toward thecentral axis 46 such that the round tubular configuration decreases in diameter along substantially all of the length of thethird section 224. - The "flared" or "bulged" shaped of the
boot 204 may help improve the transition in stiffness between thesupport 72 and theboot 204, as mentioned above. As a result, thestrain relief assembly 202 may be less likely to experience unacceptable stress concentrations when subjected to side loads or the like. - Side load performance may be even further improved by incorporating additional or alternative features on the
second section 222 of theboot 204. For example,Figs. 14 and 15 illustrate a fiber optic connector 300 ("connector 300") with astrain relief assembly 302 similar to thestrain relief assembly 202. The only difference is that thesecond section 222 of theboot 204 in thestrain relief assembly 302 includesribs 306 extending along a length of thesecond section 222. Fourribs 306 are provided in the embodiment shown, with each of theribs 306 being circumferentially aligned with one of thecorners 228 of thefirst section 220 of theboot 204. In alternative embodiments, there may be a greater or lesser number of theribs 306, and each of theribs 306 may or may not be circumferentially aligned with one of thecorners 228. Similar statements apply with respect to thecorner regions 232. That is, each of theribs 306 is circumferentially aligned with one of thecorner regions 232 in the embodiment shown, but there may more orless ribs 306 in alternative embodiments that may or may not be aligned with thecorner regions 232 of thefirst section 220. - The improved stiffness, side load performance, and other advantages may be provided without changing the spatial constraints of the strain relief assembly and/or other components of the
connector 10. For example, theshroud 120 of theconnectors strain relief assemblies boots support 72 is one way to achieve this advantage. Regardless of how the boots are received and retained on thesupport 72, a sufficient length of the boot is positioned between thefirst portion 80 of thesupport 72 and theshroud 120 so that the overall length of thestrain relief assembly 70 is not significantly increased, if at all, compared to conventional designs. In the embodiments described above, theboots front end 82 of thesupport 72 and rearwardly over the first andsecond portions boots support 72 to a lesser extent. Theboots first portion 80.
Claims (14)
- A fiber optic connector (200; 300), comprising:a ferrule (12) configured to support at least one optical fiber (16);a housing (20) from which the ferrule (12) extends;a ferrule holder (18) supporting the ferrule (12) within the housing (20);a connector body (24) coupled to the housing (20) and configured to retain the ferrule holder (18) within the housing (20), the connector body (24) having a rear portion at least partially outside of the housing (20);a crimp band (64) coupling strength members (56) of a fiber optic cable (50) to the connector body (24), wherein the crimp band (64) is positioned over a portion of the strength members (56) and an inner jacket (54) of the fiber optic cable (50); anda strain relief assembly (202; 302) positioned over the crimp band (64) and coupled to the connector body (24), the strain relief assembly (202; 302) comprising:a support (72) having a front end, a back end, and an internal cavity extending between the front end and the back end, wherein the support (72) of the strain relief assembly (202; 302) is coupled to the rear portion of the connector body (24) such that the strain relief assembly (202; 302) is coupled to the housing (20) by the connector body (24); anda boot (204) extending over at least 75% of the support (72) and rearwardly from the back end; wherein:the support (72) is formed from a first material and the boot (204) is formed from a second material that is less rigid than the first material; andthe boot (204) includes an internal passageway (210) arranged about a central axis (46) and communicating with the internal cavity of the support (72),
characterised in that:at least part of the boot (204) flares radially outward (238) from the central axis (46) as the boot (204) extends over the at least a portion of the support (72) toward the back end of the support (72); andat least part of the boot (204) tapers radially inward (224) toward the central axis (46) as the boot (204) extends rearwardly from the back end of the support (72). - The fiber optic connector (200; 300) of claim 1, wherein:the boot (204) has a width measured in a radial direction relative to the central axis (46); andthe at least a part of the boot (204) that flares radially outward (238) from the central axis (46) increases in width by at least 20%.
- The fiber optic connector (200; 300) of claim 2, wherein the at least a part of the boot (204) that tapers radially inward (224) toward the central axis (46) decreases in width by at least 50%.
- The fiber optic connector (200; 300) of any of claims 1-3, wherein:the boot (204) has a width measured in a radial direction relative to the central axis (46); andthe width is greatest at a location along the boot (204) that substantially corresponds to where the boot (204) extends over the back end of the support (72).
- The fiber optic connector (200; 300) of claim 4, wherein at the location along the boot (204) that substantially corresponds to where the boot (204) extends over the back end of the support (72), the boot has a substantially round cross-sectional profile when viewed along the central axis (46).
- The fiber optic connector (200; 300) of any of claims 1-5, wherein the boot (204) includes a distal end rearward of the support (72), and wherein the boot (204) has a substantially round tubular configuration between at least the back end of the support (72) and the distal end of the boot (204).
- The fiber optic connector (200; 300) of claim 6, wherein at least a section of the boot (204) that extends over the support (72) has a substantially rectangular tubular configuration.
- The fiber optic connector (200; 300) of claim 7, wherein at least 50% of the boot (204) that extends over the support (72) has a substantially rectangular tubular configuration.
- The fiber optic connector (200; 300) of any of claims 1-8, wherein:the support (72) includes a first portion defining the front end of the support (72) and a second portion defining the back end of the support (72), the second portion of the support (72) having a stiffness less than the first portion of the support (72);the boot (204) includes a first section (220) at least partially extending over the first portion of the support (72), a second section (222) extending over the second portion of the support (72), and a third section (224) extending rearwardly from the back end of the support (72); andthe first section, second section, and third section of the boot (204) have different tubular configurations.
- The fiber optic connector (200; 300) of claim 9, wherein:the second section of the boot (204) includes a neck portion (236) and a flared portion (238) as the second section extends over the second portion of the support (72); andthe neck portion (236) maintains a substantially constant cross-sectional profile when viewed along the central axis (46).
- The fiber optic connector (200; 300) of claim 10, wherein the neck portion (236) and the flared portion (238) have respective first and second lengths measured along the central axis (46) and wherein the first length is greater than the second length.
- The fiber optic connector (200; 300) of any of claims 9-11, wherein:the first section of the boot (204) has a substantially rectangular tubular configuration;the third section of the boot (204) has a substantially round tubular configuration; andthe second section of the boot (204) comprises at least one rib extending along a length of the second section.
- The fiber optic connector (200; 300) of claim 12, wherein:the first section of the boot (204) includes four corners (228) defined by the substantially rectangular tubular configuration of the first section; andthe at least one rib of the second section comprises four ribs (306) that are each circumferentially aligned with one of the corners of the first section.
- The fiber optic connector (200; 300) of any of claims 9-11, wherein:the first portion of the support (72) includes a plurality of projections extending through the first section of the boot (204);the plurality of projections define four corner regions (232) in the first section of the boot (204);the second section of the boot (204) comprises four ribs (306) extending along a length of the second section; andthe four ribs of the second section are circumferentially aligned with the four corner regions of the first section.
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JP4128824B2 (en) * | 2001-11-15 | 2008-07-30 | 古河電気工業株式会社 | Optical connector |
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US7001081B2 (en) * | 2003-05-22 | 2006-02-21 | 3M Innovative Properties Company | Strain relief boot with flexible extension for guiding fiber optic cable |
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US7695197B2 (en) * | 2006-04-20 | 2010-04-13 | Tyco Electronics Corporation | Bend limiter |
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US9429732B2 (en) * | 2013-05-03 | 2016-08-30 | Corning Cable Systems Llc | Fiber optic cable crimp assemblies employing integrally connected cable strain relief boots, and related fiber optic connectors, cables, and methods |
WO2015017766A1 (en) * | 2013-08-02 | 2015-02-05 | Adc Telecommunications, Inc. | Taper strain relief boot for ferrule flex connectors |
US9551842B2 (en) * | 2015-01-15 | 2017-01-24 | Corning Optical Communications LLC | Fiber optic connector with strain relief assembly |
EP3245545B1 (en) * | 2015-01-15 | 2020-09-09 | Corning Optical Communications LLC | Fiber optic connector with strain relief assembly |
-
2017
- 2017-11-13 US US15/810,981 patent/US10261268B2/en active Active
- 2017-11-14 EP EP17201750.1A patent/EP3321721B1/en active Active
- 2017-11-14 CN CN201721514900.3U patent/CN207718019U/en not_active Expired - Fee Related
Patent Citations (1)
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US6374022B1 (en) * | 1998-12-23 | 2002-04-16 | Pirelli Cavi E Sistemi S.P.A. | Bend limiting device for cables |
Also Published As
Publication number | Publication date |
---|---|
US20180136427A1 (en) | 2018-05-17 |
CN207718019U (en) | 2018-08-10 |
EP3321721A1 (en) | 2018-05-16 |
US10261268B2 (en) | 2019-04-16 |
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